(3)
 Close the protection cover to prevent the direct access to the slide control handle.

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 5. Close-up
________ Subtask 52-22-00-860-061
 A. Put the aircraft back to the serviceable condition.
 (1)
 Remove the lock pin from the inflation reservoir as follows: (Ref. Fig. 201/TASK 52-22-00-991-027)

 (a)
 Remove the lock pin from the operation valve of the inflation reservoir.

 (b)
 Put the lock pin in the stowage pocket of the inflation reservoir.

 (c)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (d)
 Install the rear inside fairing in the applicable overhead stowage compartment.

 (e)
 Close the access door of the applicable overhead stowage compartment.

 (2)
 Close the passenger/crew door (Ref. TASK 52-10-00-410-001).

 (3)
 Remove the access platform(s).

 (4)
 De-energize the ground service network
 (Ref. TASK 24-42-00-862-001).

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 TASK 52-22-00-010-002 Opening of the Emergency Exit Doors from the Outside
 1.
 Reason for the Job

__________________
 Self Explanatory

 2.
 Job Set-up Information

______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific access platform 3.20 m (10 ft. 6 in.) 98A52107632000 1 PIN - SAFETY SLIDE 98D52207551000 1 SAFETY PIN - SLIDE RELEASE LEVER
 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-42-00-861-001 Energize the Ground Service Network from the External Power 52-22-00-860-003 Special Precaution before Maintenance on the Door
 Damper and Emergency Operation Cylinder 52-22-00-991-027 Fig. 201 52-22-00-991-001 Fig. 202 52-22-00-991-002 Fig. 203
 3. Job Set-up
__________ Subtask 52-22-00-860-052
 A. Aircraft Maintenance Configuration
 (1)
 Put the access platform in position below the applicable door.

 (2)
 Energize the ground service network
 (Ref. TASK 24-42-00-861-001)

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 4. Procedure
_________ Subtask 52-22-00-010-055
 A. Opening of the Door
 (Ref. Fig. 203/TASK 52-22-00-991-002)

 (1) Look through the door window to make sure that the red warning light CABIN PRESSURE does not flash.
 WARNING : STOP THE OPENING PROCEDURE IF THE RED WARNING LIGHT
_______ FLASHES. RESIDUAL PRESSURE COULD CAUSE THE DOOR TO OPEN WITH A SUDDEN FORCE AND INJURE PERSONS AND/OR DAMAGE THE AIRCRAFT.
 (2) Push the handle flap in and pull the outboard handle away from the door.
 NOTE : The escape slide-release mechanism is automatically put in the
____
 DISARMED mode.

 (3)
 Lift the outboard handle so that the door moves up and comes free from the opening.

 (4)
 Pull the door outboard and move it forward to get access to the door damper and emergency operation cylinder.

 (5)
 Do the special precaution procedure on the door damper and emergency operation cylinder (Ref. TASK 52-22-00-860-003).

 (6)
 Move the door in the forward direction so that the door stay mechanism locks the door in its fully open position.

 Subtask 52-22-00-860-053
 B. Aircraft Maintenance Configuration
 (Ref. Fig. 201/TASK 52-22-00-991-027, 202/TASK 52-22-00-991-001)

 (1) Install the SAFETY PIN - SLIDE RELEASE LEVER (98D52207551000) in the slide release lever and the frame fitting.
 NOTE : This prevents the accidental operation of the escape
____
 slide-release mechanism.

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 Normal Operation from the Outer Side
 Figure 203/TASK 52-22-00-991-002
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1  1  May 01/04
 1  1
 1CES  1

 (2) Safety the disarmed escape slide-release mechanism as follows:
 (a)
　
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